Dynamic deployment and attitude control motion of spinning solar sail "IKAROS"

Osamu Mori; Yoji Shirasawa; Yuichi Tsuda; Ryu Funase; Takanao Saiki; Yuya Mimasu; Ryo Jifuku; Norizumi Motooka; Takayuki Yamamoto; Junichiro Kawaguchi

Dynamic deployment and attitude control motion of spinning solar sail "IKAROS"

Osamu Mori^*, Yoji Shirasawa, Yuichi Tsuda, Ryu Funase, Takanao Saiki, Yuya Mimasu, Ryo Jifuku, Norizumi Motooka, Takayuki Yamamoto, Junichiro Kawaguchi

^*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Citations (Scopus)

Abstract

In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. Multi Particle Model (MPM) and First Mode Model of out-of-plane deformation (FMM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. Considering the thruster configuration of IKAROS, the force on main body and membrane by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is simple and valid for the design of attitude controller.

Original language	English
Title of host publication	62nd International Astronautical Congress 2011, IAC 2011
Pages	5582-5588
Number of pages	7
Publication status	Published - 2011
Externally published	Yes
Event	62nd International Astronautical Congress 2011, IAC 2011 - Cape Town, South Africa Duration: 3 Oct 2011 → 7 Oct 2011

Publication series

Name	62nd International Astronautical Congress 2011, IAC 2011
Volume	7

Conference

Conference	62nd International Astronautical Congress 2011, IAC 2011
Country/Territory	South Africa
City	Cape Town
Period	3/10/11 → 7/10/11

Cite this

@inproceedings{c60e86013ae24bb8a2e552f4abd842fd,

title = "Dynamic deployment and attitude control motion of spinning solar sail {"}IKAROS{"}",

abstract = "In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. Multi Particle Model (MPM) and First Mode Model of out-of-plane deformation (FMM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. Considering the thruster configuration of IKAROS, the force on main body and membrane by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is simple and valid for the design of attitude controller.",

author = "Osamu Mori and Yoji Shirasawa and Yuichi Tsuda and Ryu Funase and Takanao Saiki and Yuya Mimasu and Ryo Jifuku and Norizumi Motooka and Takayuki Yamamoto and Junichiro Kawaguchi",

year = "2011",

language = "English",

isbn = "9781618398055",

series = "62nd International Astronautical Congress 2011, IAC 2011",

pages = "5582--5588",

booktitle = "62nd International Astronautical Congress 2011, IAC 2011",

note = "62nd International Astronautical Congress 2011, IAC 2011 ; Conference date: 03-10-2011 Through 07-10-2011",

}

Mori, O, Shirasawa, Y, Tsuda, Y, Funase, R, Saiki, T, Mimasu, Y, Jifuku, R, Motooka, N, Yamamoto, T & Kawaguchi, J 2011, Dynamic deployment and attitude control motion of spinning solar sail "IKAROS". in 62nd International Astronautical Congress 2011, IAC 2011. 62nd International Astronautical Congress 2011, IAC 2011, vol. 7, pp. 5582-5588, 62nd International Astronautical Congress 2011, IAC 2011, Cape Town, South Africa, 3/10/11.

Dynamic deployment and attitude control motion of spinning solar sail "IKAROS". / Mori, Osamu; Shirasawa, Yoji; Tsuda, Yuichi et al.
62nd International Astronautical Congress 2011, IAC 2011. 2011. p. 5582-5588 (62nd International Astronautical Congress 2011, IAC 2011; Vol. 7).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Dynamic deployment and attitude control motion of spinning solar sail "IKAROS"

AU - Mori, Osamu

AU - Shirasawa, Yoji

AU - Tsuda, Yuichi

AU - Funase, Ryu

AU - Saiki, Takanao

AU - Mimasu, Yuya

AU - Jifuku, Ryo

AU - Motooka, Norizumi

AU - Yamamoto, Takayuki

AU - Kawaguchi, Junichiro

PY - 2011

Y1 - 2011

N2 - In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. Multi Particle Model (MPM) and First Mode Model of out-of-plane deformation (FMM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. Considering the thruster configuration of IKAROS, the force on main body and membrane by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is simple and valid for the design of attitude controller.

AB - In this paper, the attitude dynamics of IKAROS, which is spinning solar sail, is presented. Multi Particle Model (MPM) and First Mode Model of out-of-plane deformation (FMM) are introduced to analyze the out-of-plane oscillation mode of spinning solar sail. Considering the thruster configuration of IKAROS, the force on main body and membrane by thruster plume as well as reaction force by thruster are integrated into MPM. The attitude motion after sail deployment or reorientation using thrusters can be analyzed by MPM numerical simulations precisely. The out-of-plane oscillation of IKAROS is governed by three modes derived from FMM. FMM is simple and valid for the design of attitude controller.

UR - http://www.scopus.com/inward/record.url?scp=84864098036&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84864098036

SN - 9781618398055

T3 - 62nd International Astronautical Congress 2011, IAC 2011

SP - 5582

EP - 5588

BT - 62nd International Astronautical Congress 2011, IAC 2011

T2 - 62nd International Astronautical Congress 2011, IAC 2011

Y2 - 3 October 2011 through 7 October 2011

ER -

Dynamic deployment and attitude control motion of spinning solar sail "IKAROS"

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